Mass equation for landing gear (FLOPS based)

[xjjiang]

Desired capability or behavior.

Copied from source code: "add in aircraft type and carrier factors as options and modify equations"

See MainGearMass of subsystem/mass/flops_based/landing_gear.py.

See NoseGearMass of subsystem/mass/flops_based/landing_gear.py.

I am not sure what this request means. We've already implemented everything from FLOPS.

Is your feature request related to a problem? Please describe.

No response

Associated Bug Report

No response